Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
A599
1737
Figure
7-4.
Clamping
Rudder
Figure
7-5.
Rudder
Pedals
Pedals
in Neutral
Position
at Neutral
Angle
1.
Place
a
bubble
protractor
against
a
rudder
pedal
steering
tube
to
check
the
neutral
angle.
(Refer
to
Figure
7-5.)
m. One
end
of each
rod
must
be disconnected
and
the
jam
nuts
loosened
to
make
any
adjustment.
Do not
attempt
to make
the
adjustment
by
means
of one
rod end
bearing,
but
divide
the
adjustment
between
the
bearings
at
each
end
of
each
rod.
Check
that
the rod
ends
have
sufficient
thread
engagement
by
ascertaining
that
a wire
will
go
through
the
check
hole
in
the
rod.
Where
no
check
holes
are
provided,
ascertain
a
minimum
of
3/8
inch
thread
engagement.
Reinstall
the rods
and tighten
the
jam
nuts.
n.
To
check
the
nose
gear
steering
for
its 22.5
°
±
2
°
maximum
right
and
left.
travel.
mark
on
each
side
of
the
nose
wheel
an angle
line
from
the
centerline
and
wheel
pivot
point.
Turn
the
wheel
to
its
maximum
travel
in
both
directions
to check
for
allowable
travel.
Should
travel
be
exceeded
in
one
direction
and
not
enough
in
the
other
direction,
check
for
possible
damage
to
the
gear
fork
or
torque
links.
7-14.
REMOVAL
OF NOSE
GEAR
DOOR
ASSEMBLY.
(Refer
to
Figure
7-6.)
a.
With
the
nose
gear
extended,
disconnect
springs
(2)
from
door
arms
(3)
by
removing
upper
attachment
hardware.
b.
Disconnect
link
assemblies
(4)
from
doors
(1)
and
remove
mechanism.
c.
To
remove
the
doors
from
cowl,
bend
the
end
of the
hinge
pin
(8)
straight
and
pull
out
the pin.
Issued:
1/3/78
LANDING
GEAR
AND
BRAKE
SYSTEM
1J22

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers